TM 1-1520-238-10
7A-11
M01-227
HOVER CEILING
100 % ROTOR RPM, ATF = 1.0
MAXIMUM TORQUE AVAILABLE (30 MIN LIMIT)
3000
12000
11000
10000
8000
9000
7000
6000
2000
4000
5000
1000
DERIVED FROM FLIGHT TEST
14000
13000
0
16000
15000
18000
17000
OGE GROSS WEIGHT
~
LB
21000
20000
19000
20000
19000
18000
17000
16000
15000
14000
13000
21000
AH-64A
CEILING/IRP
HOVER
T700-GE-701C
DATA BASIS:
REDUCE HOVER GROSS
WEIGHT 11 LB PER 1000 LB
FOR 4-TANK CONFIGURATION
NOTE:
ANTI-ICE ON, USE
FOR ENGINE INLET
NOTE:
DASHED LINES
Figure 7A-5.
Hover Ceiling Chart (Sheet 1 of 2)
